|
[Sponsors] |
May 9, 2014, 16:54 |
Quick Reference Value Question (Length)
|
#1 |
New Member
K. Smith
Join Date: Jan 2014
Posts: 5
Rep Power: 12 |
I am somewhat new to Fluent, have been using mainly EDGE in the past year. I have had an introductory course to fluent, and am now trying to improve my skills a bit. I know the reference value for length is critical in arriving at the correct Cl Cd Cm values when you set the monitors. I have a 2D 3-element airfoil (slat, main body, flap) which is extended for takeoff conditions. Do I set the reference length to be the entire length of the airfoil from leading to trailing edge, or do I sum the chord lengths of each of the 3 components? Thanks in advance.
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[swak4Foam] difficulties installing swak4foam | newbie29 | OpenFOAM Community Contributions | 120 | October 21, 2022 05:01 |
libnurbs++ | kuczmas | OpenFOAM Running, Solving & CFD | 7 | May 14, 2012 07:33 |
Question about N-S eqs. in body fixed noninertial reference frame | doctorWho | Main CFD Forum | 0 | July 12, 2011 19:07 |
OpenFoam-1.7.x on Suse 11.2 (64bit) does not compile | val46 | OpenFOAM Installation | 4 | August 27, 2010 04:43 |
Compiling new Solver with wmake | lin123 | OpenFOAM | 3 | April 13, 2010 15:18 |